Low NOx premix burner

Claim 2

A premixing burner for the combustion of fuel gas and air with reduced NO x production, said burner having a primary air-fuel gas combustion assembly and a secondary air combustion assembly, the primary air-fuel gas combustion assembly comprising a burner tube and a burner tile spaced from and surrounding the downstream end of said tube, the burner tube having a mixer connected to an extension tube and a burner tip mounted on the downstream end of said extension tube, the said mixer having inlets for fuel gas and primary air and adapted to mix said fuel and primary air prior to combustion at predetermined ratios, said burner tip having ports for passage of the gas from the extension tube, the burner tube and burner tile being adapted to support and stabilize a substoichiometric initial flame resulting from the combustion of the gases passing through the burner tip, said initial flame having a base in the region formed by said burner tile and burner tip, said secondary air combustion assembly comprising multiple secondary air ports and secondary air inlet means therefor, said secondary air ports being spaced radially from said burner tile and circumferentially from each other, the radial spacing being a sufficient distance to permit secondary air streams from the ports to react with the flame of the premixed gas substantially downstream of the burner tip, the circumferential spacing between ports being a sufficient distance to permit furnace flue gas to re-circulate to the base of the initial flame in amounts at least sufficient to achieve lower temperatures in the initial flame and to move the secondary air streams away from the initial flame, the primary air-fuel gas ratios including the range of about 25-65% of the stoichiometric air requirement of the fuel gas, the burner being adapted for a total air requirement of up to about 120 mol % of the stoichiometric air requirement of the fuel gas.

Claim 3

The burner of claim 1 wherein the secondary air ports are substantially parallel to the burner tube.

Claim 4

The burner of claim 1 wherein the secondary air ports are equidistant from the center of the burner.

Claim 5

The burner of claim 1 wherein the secondary air ports terminate downstream of the burner tile.

Claim 6

The burner of claim 1 wherein a sealing plate is disposed upstream of the burner tip and across the space between the burner tile and burner tube.

Claim 7

The burner of claim 1 wherein the secondary air inlet means includes a plenum surrounding said burner tile and air flow control device for said plenum.

Claim 8

The burner of claim 1 wherein said mixer is in the form of a jet eductor for inspirating and mixing primary air and fuel gas.

Claim 9

The burner of claim 1 wherein the jet eductor includes an inlet pipe for fuel gas at high pressure, an orifice on said pipe to provide one or more jets of fuel gas and a venturi pipe to receive said fuel gas and inspirate air therewith.

Claim 10

A furnace having walls, a top and a floor and containing at least one premixing burner for the combustion of fuel gas and air with reduced NO x production, said burner having a primary air-fuel gas combustion assembly and a secondary air combustion assembly, the primary air-fuel gas combustion assembly comprising a burner tube and a burner tile spaced from and surrounding the downstream end of said tube, the burner tube having a mixer connected to an extension tube and a burner tip mounted on the downstream end of said extension tube, the said mixer having inlets for fuel gas and primary air and adapted to mix said fuel gas and primary air prior to combustion at predetermined ratios, said burner tip having ports for passage of the gas from the extension tube, the burner tube and burner tile being adapted to support and stabilize a substoichiometric initial flame resulting from the combustion of the gases passing through the burner tip, said initial flame having a base in the region formed by said burner tile and burner tip, said secondary air combustion assembly comprising multiple secondary air ports and secondary air inlet means therefor, said secondary air ports being spaced radially from said burner tile and circumferentially from each other, the radial spacing being a sufficient distance to permit secondary air streams from the ports to react with the flame of the premixed gas substantially downstream of the burner tip, the circumferential spacing between ports being a sufficient distance to permit furnace flue gas to re-circulate to the base of the initial flame in amounts at least sufficient to achieve lower temperatures in the initial flame and to move the secondary air streams away from the initial flame, the primary air-fuel gas ratios including the range of about 25-65% of the stoichiometric air requirement of the fuel gas, the burner being adapted for a total air requirement of up to about 120 mol% of the stoichiometric air requirement of the fuel gas.

Claim 11

A furnace having walls, a top and a floor and containing at least one premixing burner for the combustion of fuel gas and air with reduced NO x production, said burner having a primary air-fuel gas combustion assembly and a secondary air combustion assembly, the primary air-fuel gas combustion assembly comprising a burner tube and a burner tile spaced from and surrounding the downstream end of said tube, the burner tube having a mixer connected to an extension tube and a burner tip mounted on the downstream end of said extension tube, the said mixer having inlets for fuel gas and primary air and adapted to mix said fuel gas and primary air prior to combustion at predetermined ratios, said burner tip having ports for passage of the gas from the extension tube, the burner tube and burner tile being adapted to support and stabilize a substoichiometric initial flame resulting from the combustion of the gases passing through the burner tip, said initial flame having a base in the region formed by said burner tile and burner tip, said secondary air combustion assembly comprising multiple secondary air ports and secondary air inlet means therefor, said secondary air ports being spaced radially from said burner tile and circumferentially from each other, the radial spacing being a sufficient distance to permit secondary air streams from the ports to react with the flame of the premixed gas substantially downstream of the burner tip, the circumferential spacing between ports being a sufficient distance to permit furnace flue gas to re-circulate to the base of the initial flame in amounts at least sufficient to achieve lower temperatures in the initial flame and to move the secondary air streams away from the initial flame, the primary air-fuel gas ratios including the range of about 25-65% of the stoichiometric air requirement of the fuel gas, the burner being adapted for a total air requirement of up to about 120 mol% of the stoichiometric air requirement of the fuel gas.

Claim 12

The furnace of claim 9 in which at least one of said premixing burner is located in the floor of said furnace.

Claim 13

The furnace of claim 9 in which at least one of said premixing burner is located in the walls of said furnace.

Claim 14

The furnace of claims 9, 10 and 11 wherein the furnace includes coils adapted for steam cracking of olefins and said coils are disposed from top to floor of said furnace.

Claim 15

In a method for heating a furnace by combustion of fuel gas and air at ratios of upto about 120 mol% of stoichiometric air requirement, the improvement comprising conducting said combustion in spaced sequential steps while reducing the production of NO x in said combustion, said stages being: (a) A premixed primary air-fuel gas combustion stage wherein primary air is added to fuel gas at ratios of about 25 to 65% of stoichiometric air requirement, the same are mixed to form a homogeneous gas mixture, the mixture is passed through a burner tube and then combusted to form an initial flame that is stabilized and supported by the burner tube and a burner tile surrounding the burner tube and furnace flue gas is recirculated to the base of the initial flame, (b) A secondary air combustion stage wherein secondary air is separated into individual air streams, the streams of secondary air flow to the initial flame at a position substantially downsteam of the base of the initial flame while furnace flue gas recirculates between the streams to the base of the initial flame and the secondary air reacts with the fuel gas remaining in the initial flame to complete the combustion thereof, the volume of furnace flue gas recirculating to the base of the initial flame during said stages being sufficient to lower the flame temperature of the initial flame and to maintain the secondary air streams away from the premixed primary air-fuel gas combustion stage.

Claim 16

In a method for heating a furnace by combustion of fuel gas and air at ratios of upto about 120 mol% of stoichiometric air requirement, the improvement comprising conducting said combustion in spaced sequential steps while reducing the production of NO x in said combustion, said stages being: (a) A premixed primary air-fuel gas combustion stage wherein primary air is added to fuel gas at ratios of about 25 to 65% of stoichiometric air requirement, the same are mixed to form a homogeneous gas mixture, the mixture is passed through a burner tube and then combusted to form an initial flame that is stabilized and supported by the burner tube and a burner tile surrounding the burner tube and furnace flue gas is recirculated to the base of the initial flame, (b) A secondary air combustion stage wherein secondary air is separated into individual air streams, the streams of secondary air flow to the initial flame at a position substantially downsteam of the base of the initial flame while furnace flue gas recirculates between the streams to the base of the initial flame and the secondary air reacts with the fuel gas remaining in the initial flame to complete the combustion thereof, the volume of furnace flue gas recirculating to the base of the initial flame during said stages being sufficient to lower the flame temperature of the initial flame and to maintain the secondary air streams away from the premixed primary air-fuel gas combustion stage.

Claim 17

The method of claim 13 in which the air for the primary air and the secondary air is selected from the group consisting of ambient air, preheated air and gas turbine exhaust.

Claim 18

The method of claim 13 wherein the ratio of primary air to fuel gas is at about the fuel-rich, upper limit of flammability.

Claim 19

The method of claim 13 wherin the fuel gas comprises natural gas and the ratio of primary air to fuel gas is about 45% to about 50% of the stoichiometric air requirement.

Claim 20

The method according to claim 13 wherein the furnace is a steam cracking furnace.